|Publication number||US7215840 B2|
|Application number||US 11/388,568|
|Publication date||May 8, 2007|
|Filing date||Mar 23, 2006|
|Priority date||Dec 14, 2001|
|Also published as||US7110624, US7133583, US7197200, US7327909, US20040179766, US20060165338, US20060165339, US20060177170, US20060177171, WO2005094262A2, WO2005094262A3|
|Publication number||11388568, 388568, US 7215840 B2, US 7215840B2, US-B2-7215840, US7215840 B2, US7215840B2|
|Inventors||David Marceau, Dennis F. Elkins, Forrest L. Williams, Allen H. Tanner|
|Original Assignee||Evans & Sutherland Computer Corporation|
|Export Citation||BiBTeX, EndNote, RefMan|
|Patent Citations (22), Referenced by (5), Classifications (18), Legal Events (7)|
|External Links: USPTO, USPTO Assignment, Espacenet|
The present application is a divisional of U.S. patent application Ser. No. 10/807,808, filed Mar. 23, 2004 now U.S. Pat. No. 7,110,624, which is a continuation-in-part of U.S. patent application Ser. No. 10/017,162, filed Dec. 14, 2001 now U.S. Pat. No. 6,763,042, and a continuation-in-part of U.S. patent application Ser. No. 10/383,909, filed Mar. 6, 2003 now U.S. Pat. No. 6,868,212.
1. Field of the Invention
The present invention relates generally to tuning of optical fiber structures. More particularly, the present invention relates to tuning, protection, and environmental isolation of distributed feedback fiber lasers.
2. Related Art
Lasers have found use in a variety of applications, including displays, optical printing, optical recording, and communications. Distributed feedback (DFB) fiber lasers, in particular, have proven useful in those applications where the single-mode operation, narrow optical linewidth, and low noise performance of DFB fiber lasers are particularly advantageous. Tuning of DFB fiber laser optical frequency is generally required to correct initial manufacturing tolerances, and various fixed schemes to accomplish initial tuning are known. In many applications, very stable laser optical frequency is required, however, and maintaining long-term stability has proved challenging.
Controlled changes in temperature or controlled application of mechanical strain to the fiber may be used to tune the optical frequency of a DFB fiber laser. Changes in temperature and mechanical strain result in changes to the period of gratings impressed into the fiber resulting in a change in the optical frequency of the DFB fiber laser. Thermal tuning by adjusting the temperature of a DFB fiber laser is limited to slow laser optical frequency changes, however, due to slow change rates of the thermal mass of the fiber and associated temperature control mechanism.
Although mechanical tuning of a DFB fiber laser by the application of mechanical strain can accomplish rapid changes in the laser optical frequency, such tuning is difficult. The DFB fiber laser manufacturing process weakens the fiber permitting excessive tension to break the fiber. Similarly, wide range mechanical tuning of the fiber can reduce reliability due to the increased chance of fiber breakage. Although some of the problems associated with mechanical tuning can be avoided by limiting the applied mechanical strain to compression loading rather than tension, application of compression to a fiber is difficult to achieve without buckling the fiber. Hence, complex mechanical structures are required to prevent buckling when applying compression-only mechanical tuning.
It has been recognized that it would be advantageous to develop a technique to provide wide range and rapid tuning of the optical frequency of a fiber optic component simultaneously. Furthermore, it has been recognized that it would be advantageous to provide tuning of the optical frequency of a fiber optic component while also providing protection of the fiber optic component and isolation of the fiber optic component from acoustic vibration and mechanical shock. Furthermore, it is desirable to accomplish these objectives using a less complex structure than prior art mechanically tuned lasers.
The invention provides a fiber optic component tuning and isolating support device. The support device includes a tensioning structure in thermal contact with a thermal control structure which includes a thermally-conductive, acoustic-damping material and a thermally-controlled surface. In another embodiment, the invention provides a fiber optic component tuning and isolating support device which includes a thermally-conductive, acoustic-damping material in thermal contact with a thermally-controlled surface and configured to receive a fiber optic component. In another embodiment, the invention provides a fiber optic component tuning and isolating device which includes a tensioning structure encased in an acoustic-damping material.
The invention also provides a method of substantially simultaneously thermally and mechanically tuning a fiber optic component. Another embodiment of the invention also provides a method of compensating variations in an optical system by thermally and mechanically tuning the optical frequency of a DFB fiber laser.
Finally, the invention also provides a method of making a tunable fiber optic component by encasing a fiber optic component in a tensioning structure and affixing the tensioning structure to a thermally-controlled surface using a thermally-conductive, acoustic-damping material.
Additional features and advantages of the invention will be apparent from the detailed description which follows, taken in conjunction with the accompanying drawings, which together illustrate, by way of example, features of the invention.
Reference will now be made to the exemplary embodiments illustrated in the drawing, and specific language will be used herein to describe the same. It will nevertheless be understood that no limitation of the scope of the invention is thereby intended. Alterations and further modifications of the inventive features illustrated herein, and additional applications of the principles of the inventions as illustrated herein, which would occur to one skilled in the relevant art and having possession of this disclosure, are to be considered within the scope of the invention.
A system for simultaneous thermal tuning and mechanical tuning of a fiber optic component with integrated physical protection and environmental isolation, in accordance with an embodiment of the present invention, is illustrated in
In accordance with one aspect of the present invention, the tensioning structure 14 may be fabricated of a piezoelectric material 32 shaped in the form of a tube. As illustrated in
This mechanical tuning using the tensioning structure 14 can provide small optical frequency changes of a DFB fiber laser up to a few GHz. The rate at which frequency changes may be tuned is quite rapid: tuning rates of up to several hundred kHz may be obtained, depending primarily on the mechanical frequency response of the tensioning structure, as is discussed further below.
Further detail of the attachment of the fiber optic component 12 and electrical activation of the tensioning structure 14 is shown in the alternate embodiments illustrated in cross sectional views
Alternately, as illustrated in
Optionally, the area within the bore 41 of the tensioning structure 14 may be filled with a thermally-conductive, acoustic-damping material, such as oil 42. This will further enhance the acoustic isolation of the fiber optic component.
Various other arrangements of the electrical connection to the electrodes are also possible. As illustrated in
It is desirable that the tensioning structure extends longitudinally to completely encompass the active region of a DFB fiber laser to ensure that uniform stress is applied to the gratings of the DFB fiber laser and to fully protect the DFB fiber laser. If the tensioning structure is designed to enclose only a portion of the active region of a DFB fiber laser, this may result in poor efficiency or even bimodal output from the laser if stretched and unstretched portions of the DFB fiber laser have different grating periods.
The tensioning structure 14 may be fabricated entirely of a piezoelectric or other similar material that provides electrically activated mechanical translation. Alternately, as shown in
In accordance with another aspect of the present invention, thermal tuning of the optical frequency may be concurrently accomplished by varying the temperature of the fiber optic component with a thermal control structure. As illustrated in
Thermal tuning using the thermally-controlled surface can provide large optical frequency changes up to several 100 GHz, complementing the narrower tuning range provided by mechanical tuning using the tensioning structure. The tuning rate of the thermally-controlled surface 18 is smaller than the mechanical tuning rate, allowing changing the optical frequency of the laser at tuning rates of up to about 5 Hz. Accordingly, the present invention provides both coarse tuning and fine tuning within the same structure.
The invention also solves problems inherent in trying to provide physical protection and environmental isolation of a tunable laser. The tensioning structure 14 provides physical protection to fragile fiber optic components. The tensioning structure may also provide the ability to mechanically tune the laser without requiring hard mounting of the fiber optic component to any other structure than the tensioning structure. The tensioning structure, containing the DFB fiber laser 12, may thus be mechanically isolated using thermally-conductive, acoustic-damping material 16. The acoustic-damping property isolates the DFB fiber laser from acoustic vibration and mechanical shock in the surrounding environment. The thermally-conductive property thermally couples the DFB fiber laser 12 to the thermally-controlled surface 18, ensuring that the DFB fiber laser 12 maintains substantially the same temperature as the thermally-controlled surface 18 and thus isolating the DFB fiber laser 12 from ambient environmental temperature changes. If temperature control is not required, an acoustic-damping material may be used instead of the thermally-conductive, acoustic-damping material. Conversely, if isolation from shock and vibration is not required, a thermally-conductive material may be used instead of the thermally-conductive, acoustic-damping material.
Although the DFB fiber laser 12 may respond to pressure changes in the environment, these changes are slow and can be compensated by the thermal tuning. Hence, environmental isolation from ambient temperature and mechanical shock and vibration is provided.
An alternate embodiment of a system for simultaneous thermal tuning and mechanical tuning of a fiber optic component with integrated physical protection and environmental isolation is illustrated in
Alternately, in accordance with another aspect of the present invention, the tensioning structure may be implemented as an open structure, giving up some physical protection of the fiber optic component for enhanced thermal coupling. For example, as illustrated in
In accordance with yet another aspect of the present invention, the tensioning structure may be implemented as a mounting plate. For example, as illustrated in
An important aspect of the present invention is the length of the fiber optic component. For example, a DFB fiber laser will exhibit a mechanical natural frequency that depends on its length. Longer lasers exhibit a lower mechanical natural frequency; shorter lasers exhibit a higher mechanical natural frequency. If the mechanical natural frequency of the laser is too low, the mechanical tuning of the laser may perform poorly. Additionally, if the mechanical natural frequency of the laser is below about 20 kHz, the laser may be excessively responsive to acoustic vibration and mechanical shock, and it may prove difficult to maintain a stable optical frequency.
On the other hand, the optical gain and optical linewidth of the laser also depend on the length of the laser. Longer lasers provide greater optical gain and narrower optical linewidth; shorter lasers provide less optical gain and wider optical linewidth. Depending on the particular application, an optimal length may therefore exist which balances a desire for a relatively high mechanical natural frequency with a desire for relatively narrow optical linewidth. A DFB fiber laser length of about 15 mm has proven advantageous, although lengths of about 10 mm to 50 mm may also prove useful, depending upon the particular application.
In accordance with another aspect of the current invention, thermal tuning using the thermally-controlled surface 18 may be accomplished simultaneously with mechanical tuning using the tensioning structure 14. Mechanical tuning can provide small optical frequency changes at high rates; conversely, thermal tuning can provide large optical frequency changes at low rates. The combination of thermal tuning and mechanical tuning thus provides a wide optical frequency tuning range without encountering the problem of reduced reliability, since the mechanical strain on the laser is limited to a small range. Large optical frequency changes are accomplished using the thermal tuning, avoiding the need to overstress the fiber. The invention also avoids the limited tuning speed that thermal tuning alone provides by including simultaneous mechanical tuning. By combining both types of tuning in a single structure, the invention provides a more versatile fiber optic tuning structure using fewer parts. Furthermore, improved isolation from environmental effects, such as acoustic vibration, mechanical shock, and temperature variations is provided.
The simultaneous wide optical frequency range and rapid tuning rate of DFB fiber laser optical frequency provided by the present invention may be used to improve performance of optical systems. For example, when using resonant optical cavity injection, such as that disclosed by co-pending U.S. patent application Ser. No. 10/017,162, herein incorporated by reference, it is necessary that the laser optical frequency and cavity optical resonant frequency be precisely matched to obtain efficient operation. Both laser optical frequency and cavity optical resonant frequency can, however, be affected by a variety of factors, including temperature changes, mechanical drift and creep, mechanical shock, and acoustic vibration. This matching can be accomplished with the present invention, for example, by tuning the laser optical frequency to match the resonance of the cavity. Thermal tuning may adjust the DFB fiber laser optical frequency to match slow changes in the resonant frequency of the cavity optical resonant frequency caused by, for example, temperature changes, pressure changes, mechanical drift, or mechanical creep. Rapid mechanical tuning may adjust the DFB fiber laser optical frequency to match the rapid changes in cavity resonant frequency caused by, for example, acoustic vibration, mechanical vibration, or mechanical shock. Furthermore, thermal tuning may also be used to compensate any slow drift in the DFB fiber laser optical frequency caused by, for example, mechanical creep or ambient pressure changes.
It is to be understood that the above-referenced arrangements are illustrative of the application for the principles of the present invention. Numerous modifications and alternative arrangements can be devised without departing from the spirit and scope of the present invention while the present invention has been shown in the drawings and described above in connection with the exemplary embodiments(s) of the invention. It will be apparent to those of ordinary skill in the art that numerous modifications can be made without departing from the principles and concepts of the invention as set forth in the claims.
|Cited Patent||Filing date||Publication date||Applicant||Title|
|US4636031||Oct 28, 1983||Jan 13, 1987||Chevron Research Company||Process of tuning a grated optical fiber and the tuned optical fiber|
|US5005005 *||Mar 1, 1989||Apr 2, 1991||Brossia Charles E||Fiber optic probe system|
|US5047626 *||Jan 3, 1990||Sep 10, 1991||The United States Of America As Represented By The Secretary Of The Navy||Optical fiber sensor for measuring physical properties of liquids|
|US5115127 *||Sep 17, 1990||May 19, 1992||The United States Of America As Represented By The Secretary Of The Navy||Optical fiber sensor for measuring physical properties of fluids|
|US5159601||Jul 17, 1991||Oct 27, 1992||General Instrument Corporation||Method for producing a tunable erbium fiber laser|
|US5317576||Feb 1, 1993||May 31, 1994||United Technologies Corporation||Continously tunable single-mode rare-earth doped pumped laser arrangement|
|US5536085||Mar 30, 1995||Jul 16, 1996||Northern Telecom Limited||Multi-wavelength gain-coupled distributed feedback laser array with fine tunability|
|US5551283 *||Aug 3, 1994||Sep 3, 1996||Ricoh Seiki Company, Ltd.||Atmosphere measuring device and flow sensor|
|US5691999||Sep 30, 1994||Nov 25, 1997||United Technologies Corporation||Compression-tuned fiber laser|
|US6263002||Sep 4, 1998||Jul 17, 2001||Micron Optics, Inc.||Tunable fiber Fabry-Perot surface-emitting lasers|
|US6381385 *||Dec 22, 1999||Apr 30, 2002||Nortel Networks Limited||Polarization mode dispersion emulation|
|US6393181||Jun 18, 1998||May 21, 2002||Jds Uniphase Pty. Ltd.||Temperature stable Bragg grating package with post tuning for accurate setting of centre frequency|
|US6449293||May 15, 2000||Sep 10, 2002||Ionas A/S Birkerod||Temperature stabilization of optical waveguides|
|US6452667||Dec 6, 1999||Sep 17, 2002||Weatherford/Lamb Inc.||Pressure-isolated bragg grating temperature sensor|
|US6470036||Nov 3, 2000||Oct 22, 2002||Cidra Corporation||Tunable external cavity semiconductor laser incorporating a tunable bragg grating|
|US6480513||Oct 3, 2000||Nov 12, 2002||K2 Optronics, Inc.||Tunable external cavity laser|
|US6490931||Sep 20, 1999||Dec 10, 2002||Weatherford/Lamb, Inc.||Fused tension-based fiber grating pressure sensor|
|US6519388||Dec 6, 1999||Feb 11, 2003||Cidra Corporation||Tube-encased fiber grating|
|US6534248||Jan 24, 2001||Mar 18, 2003||Science And Technology Corporation @ Unm||Tunable bragg grating and devices employing the same|
|US6563968||Sep 10, 2001||May 13, 2003||Cidra Corporation||Tunable optical structure featuring feedback control|
|US6776045 *||Nov 8, 2001||Aug 17, 2004||Cidra Corporation||Bragg grating pressure sensor for industrial sensing applications|
|US20020154860 *||Nov 8, 2001||Oct 24, 2002||Fernald Mark R.||Bragg grating pressure sensor for industrial sensing applications|
|Citing Patent||Filing date||Publication date||Applicant||Title|
|US7891818||Dec 12, 2007||Feb 22, 2011||Evans & Sutherland Computer Corporation||System and method for aligning RGB light in a single modulator projector|
|US8077378||Nov 12, 2009||Dec 13, 2011||Evans & Sutherland Computer Corporation||Calibration system and method for light modulation device|
|US8358317||May 26, 2009||Jan 22, 2013||Evans & Sutherland Computer Corporation||System and method for displaying a planar image on a curved surface|
|US8702248||Jun 11, 2009||Apr 22, 2014||Evans & Sutherland Computer Corporation||Projection method for reducing interpixel gaps on a viewing surface|
|US9641826||Jul 10, 2012||May 2, 2017||Evans & Sutherland Computer Corporation||System and method for displaying distant 3-D stereo on a dome surface|
|U.S. Classification||385/12, 385/13|
|International Classification||H01S5/12, H01S5/06, G02B6/02, G02B6/26, G02B6/00|
|Cooperative Classification||G02F1/0134, H01S5/0612, H01S5/12, G02F1/0115, G02B6/02171, G02F1/0147, G02F2201/307, G02B6/022|
|European Classification||G02B6/02G8T2, G02B6/02G8R, G02F1/01C5|
|Dec 13, 2010||REMI||Maintenance fee reminder mailed|
|Feb 22, 2011||SULP||Surcharge for late payment|
|Feb 22, 2011||FPAY||Fee payment|
Year of fee payment: 4
|Dec 19, 2014||REMI||Maintenance fee reminder mailed|
|May 8, 2015||LAPS||Lapse for failure to pay maintenance fees|
|Jun 30, 2015||FP||Expired due to failure to pay maintenance fee|
Effective date: 20150508
|Jul 22, 2015||AS||Assignment|
Owner name: PENSION BENEFIT GUARANTY CORPORATION, DISTRICT OF
Free format text: SECURITY INTEREST;ASSIGNORS:EVANS & SUTHERLAND COMPUTER CORPORATION;SPITZ, INC.;REEL/FRAME:036149/0501
Effective date: 20150721